Douglas DC-9-41
Service difficulty reports · 2,671
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC941' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC941' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA9500807Longeron · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CORRODED BETWEEN FS 879 AND FS 1031. REPLACED LONGERON 30 SECTION IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR 9510979755Skin · crackedDURING PERIORIC CHECK, FOUND A CRACK IN THE EXTERNAL POWER RECEPTACLE CAVITY FORWARD LOWER CORNER. REPAIRED PER EA 97-98402.SDR 9509699758Epr Transmitter · malfunctionedNR 2 ENGINE EPR INDICATION BEGAN DECREASING SHORTLY AFTER DEPARTURE. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE EPR TRANSMITTER. THE AIRCRAFT WAS RUNUP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500825Fitting · corrodedWHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER, LEFT INBOARD HINGE ATTACH LUG ON THE VERTICAL STABILIZER CORRODED IN THE BEARING BORE. REPAIRED IAW ABX REA D955-11-55-MR.SDR ABXA9500987Skin · corrodedDURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE CENTER SKIN. REPLACED CENTER SKIN IAW DC-9 SRM 55-21-0.SDR ABXA9500986Skin · corrodedDURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE LOWER OUTBOARD SKIN AROUND DOUBLERS. REPLACED SKIN IAW DC-9 SRM 55-21-0.SDR 9510949755Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 30 AFT OF FS 973. REPAIRED PER EA 97-98399.SDR 9509989752Wire · brokenLOSS OF LEFT GENERATOR WITH CROSSTIE LOCKOUT OCCURRED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO GATE. FOUND BROKEN WIRE AT TERMINAL ON LEFT GENERATOR CURRENT TRANSFORMER. INSTALLED NEW TERMINAL. OPERATIONAL CHECK OK, AIRCRAFT RETURNESDR ABXA9500786Pan · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR JAMB PAN DENTED AT BAYONET FITTING. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11734-MR.SDR ABXA9500796Window Belt · misdrilledDURING D-CHECK ACCEPTANCE INSPECTION, FOUND DURING REPLACEMENT OF WINDOW BELT PANEL, THAT THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE AT FS 465R. REPAIRED WINDOW BELT PANEL IAW ABX REA D953-11822-MR.SDR ABXA9500791Blkhd Web · chafedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD CHAFED ON THE LEFT SIDE BELOW THE LOWER FIRE EXTINGUISHER BOTTLE. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-11758-MR.SDR ABXA9500789Pan · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR PAN REQUIRED REPAIR DUE TO ACCOMPLISHMENT OF CUSP ANGLE REPAIRS. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11737-MR.SDR ABXA9500535Eel Power Supply · defectiveEMERGENCY LIGHTS COME ON WHEN POWER IS TURNED OFF. REPLACED EMERGENCY LIGHTS POWER PACK. OPS CHECKED GOOD IAW DC-9 M.M., CHAPTER 33.SDR 9509379752Wire · brokenSHORTLY AFTER TAKEOFF, LEFT GENERATOR OFF, DC BUS OFF, LEFT AC BUS OFF, AND AC CROSSTIE LOCKOUT LIGHTS ILLUMINATED. INITIATED COCKPIT OPERATING MANUAL PROCEDURES AND TRIED RESTORING GENERATOR BACK ON LINE WITH NO SUCCESS. FLIGHT RETURNED TO YEG AND LANDED WISDR ABXA9500808Longeron · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 BLENDED. CORROSION WAS BEYOND SRM LIMITS AT FS 794. REPLACED LONGERON 30 IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-5 AND 51-10-4.SDR ABXA9500804Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT LOWER CARGO COMPARTMENT FORWARD EXTERIOR SKIN FROM LONGERON 26L TO 26R CORRODED FROM FS 794 TO FS 879. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-104, 51-30-2 AND 51-30-5 AND PFEA D953-9883.SDR ABXA9500792Fitting · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT ATTACH FITTINGS ON THE VERTICAL STABILIZER GOUGED AT HORIZONTAL STABILIZER JACKSCREW GIMBAL ATTACH POINTS. REPAIRED FITTINGS IAW ABX REA D955-11779-MR.SDR ABXA9500744Blkhd Fastener · mislocatedDURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, VERTICAL BRACE, LOWER FASTENER, HAD IMPROPER EDGE DISTANCE ON THE LEFT SIDE. REPAIRED BRACE IAW ABX REA D953-11754.SDR ABXA9500793Window Belt · misdrilledDURING D-CHECK ACCEPTANCE INSPECTION, WHILE REPLACING THE WINDOW BELT PANEL AT FS 389, FOUND THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE. REPAIRED WINDOW BELT IAW ABX REA D953-11780-MR.SDR ABXA9500745Door Arm · wornDURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY ON FLYING DOOR ARM. REPLACED RIGHT MAIN LANDING GEAR DOOR ARM ASSEMBLY AND BEARINGS IAW DC-9 M.M., CHAP. 32-10-6.SDR ABXA9500803Trunnion Fitting · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT MAIN LANDING GEAR TRUNNION FITTING CORRODED AT THE FORWARD ATTACH LUG. REPLACED TRUNNION FITTING IAW ABX EA SB57-03131-MA.SDR 95ZZZX3404Jamb · crackedDURING CHECK C, FOUND A 1.25 INCH RADIAL CRACK AT TOP LEFT SIDE OF AFT VENTRAL DOOR JAMB, RUNNING CIRCUMFERENTIALLY IN RADIUS OF DASH 13 ANGLE. STOP DRILLED PER EMLR NR 65704 AND REPLACED FASTENERS PER SRM CHAPTER 51 AND TWA STANDARD PRACTICES. AIRCRAFT TOTASDR ABXA9500788Intercostal · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN INTERCOSTAL AT FS 180 AND BL 0 TO LBL 22 HAD AN IMPROPER REPAIR. REPAIRED IAW ABX REA D953-11736-MR.SDR ABXA9500787Stringer · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEFT WING STRINGER NR 26 HAD PREVIOUS REPAIR AT XRS 200 THAT WAS NOT IAW THE SRM. REPAIRED LEFT WING STRINGER IAW ABX REA D957-11735-MR.SDR ABXA9500784Window Belt · misdrilledDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WINDOW BELT SECTION FROM FS 541 TO FS 636 HAD SHORT RIVET EDGE DISTANCE ON ONE FASTENER. REPLACED WINDOW BELT SECTION IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND REPAIRED SHORT EDGE DISTANCE AREA IAW ABX REASDR ABXA9500783Floorbeam · chafedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A FLOORBEAM CHAFED AT FS 200 IN THE MAIN CABIN. REPAIRED FLOORBEAM AT FS 200 IAW ABX REA D953-11699-MR.SDR ABXA9500742Intercostal · crackedDURING D - CHECK INSPECTION, FOUND THE UPPER SIDE CRACKED ON AN INTERCOSTAL, BETWEEN FS 37 AND FS 44. REPLACED INTERCOSTAL IAW DC-9 SRM, CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9500628Tr Link · crackedDURING COMPLIANCE OF A.D. 75-14-06, A.D. 90-18-03; S.B.'S 78-36, 78-40 AND 78-66, FOUND CRACK INDICATION ON RIGHT ENGINE LOWER INBOARD THRUST REVERSER DRIVER LINK. REPLACED DRIVER LINK IAW DC-9 M.M. 78-31-5. SHOP FINDING: LINK CRACKED. SCRAPPED LINK.SDR ABXA9500785Pan · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR PAN DENTED AND BOWED. ALSO, THERE WERE SOME DOUBLE DRILLED RIVET HOLES. REPAIRED FORWARD LOWER DOOR JAMB PAN IAW ABX REA D953-11714-MR.SDR ABXA9500815Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUSLY INSTALLED RIGHT SKIN DOUBLER CRACKED AT AFT HINGE OF RIGHT NOSE LANDING GEAR AFT DOOR. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-10-2.SDR ABXA9500741Retainer · crackedDURING D - CHECK INSPECTION, FOUND THE LEFT WINDOW SEAL RETAINER CRACKED IN THE UPPER FORWARD CORNER AT FS 680. REPAIRED IAW ABX REA D953-11589.SDR ABXA9500816Pylon Blkhd · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT PYLON BULKHEAD CRACKED SEVERAL PLACES AT FS 1041. REPLACED BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND DOUGLAS DRAWING NR 9912243.SDR ABXA9500814Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1231 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9500805Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244, CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500806Skin · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT VERTICAL STABILIZER SKIN GOUGED UNDER THE LOWER HORIZONTAL STABILIZER FAIRING. REPLACED VERTICAL STAB SKIN IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500809Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE PANEL FROM FS 1197 TO 1231 CORRODED BELOW THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500743Blkhd Angle · damagedDURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, LOWER ATTACH ANGLE FASTENER HOLES OVERSIZED ON THE LEFT SIDE. REPLACED ATTACH ANGLE IAW DC-9 SRM, CHAPTER 51-30-4.SDR ABXA9500812Angle · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT PYLON WEB UPPER ATTACH ANGLE CRACKED. REPLACED UPPER WEB ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9500555Skin · wrinkledDURING C-CHECK INSPECTION, FOUND EXTERIOR SKIN WRINKLED AT STA 945 TO 965, LONGERON 25R. REPAIRED ABX REA D953-11561-MR.SDR ABXA9500554Frame · crackedDURING C-CHECK INSPECTION, FOUND FRAME 1072 CRACKED AT LONGERON 7R. REPAIRED FRAME IAW ABX REA D953-11564-MR.SDR ABXA9500810Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500553Drive Link · crackedDURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND OUTBOARD LOWER THRUST REVERSER DRIVE LINK HAD A CRACK INDICATION. REPLACED OUTBOARD LOWER THRUST REVERSER DRIVE LINK IAW DC-9 MM 78-32, LINK WAS SCRAPPED.SDR ABXA9500383Eel Battery · dischargedEMERGENCY LIGHTS VERY DIM. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM CHAPTER 33. OPS CHECKED GOOD.SDR ABXA9500811Eyebrow Window · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CAPTAIN'S EYEBROW WINDOW DELAMINATED. REPLACED CAPTAIN'S EYEBROW WINDOW IAW DC-9 MM CHAPTER 56-10-4.SDR 9507369751Indication · malfunctionedDURING CLIMBOUT FROM DTW, ALL THREE LANDING GEAR RED UNSAFE LIGHTS AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO DESTINATION (CMH) AND LANDED WITHOUT INCIDENT. INSPECTED GSDR 9507359754Gen Contl Panel · malfunctionedLEFT AC GENERATOR DROPPED OFF LINE WITH ASSOCIATED CROSSTIE LOCKOUT DURING TAKEOFF ROLL AT 50 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED THE LEFT GENERATOR CONTROL PANEL. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 9507279759Handle · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ALSO, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE CLIPS AND LATCHES. CHSDR 9506939759Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FORWARD AND AFT SIDES OF THE MAIN LANDING GEAR FIXED SIDE BRACE ATTACH FITTING LUG. REWORKED LUG PER EA 97-097473.SDR ABXA9500351Control Box · defectiveALL FOUR ANTI-SKID LIGHTS ILLUMINATED AFTER GEAR EXTENSION. RECYCLED SWITCH AND CHECKED CIRCUIT BREAKERS. NO EFFECT. LIGHTS WENT OUT ON THEIR OWN ABOUT TWO MINUTES LATER. ALSO RECYCLED GEAR. REPLACED ANTI-SKID CONTROL BOX IAW DC-9 MM 32-43-4. OPS CHECKED SDR 9506919762Fitting · crackedDURING LINE CHECK, FOUND CRACK IN THE RIGHT TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REPLACED FITTING PER SRM 51-30-1.
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